# N994FD: Boeing 757-23A - Status: Valid registration - Airframe: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (registry code 1384967, 178 seats) - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (The Boeing Company) (OpenAirDocs) - Serial number: 25490 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: May 22, 2008 - Expires: June 30, 2027 - Mode S code: ADE200 - Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=994FD - Page: https://openairdocs.org/aircraft/N994FD From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Boeing 757-23A) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N994FD. ## FAA accident and incident reports None matched to N994FD. ## Service difficulty reports (72, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA202208031840](https://openairdocs.org/sdr/FDEA202208031840), Aug 3, 2022: FITTING. DETACHED. R1 DOOR SLIDE WOULD NOT ARM. ARMING HANDLE WILL NOT FULLY DISARM. REATTACHED GRIT BAR FITTING IAW B757 AMM 25-66-10-2, OPS CHECK GOOD, A/C OK FOR SERVICE. - [SDR FDEA202112270006](https://openairdocs.org/sdr/FDEA202112270006), Dec 27, 2021: NONE. NONE. MAIN CARGO FLOOR SEAT TRACK LOBE DAMAGED AT STA 579 AT BL45L. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA.440-STA. 690 LBL 45.5 IN REF TO 757 SRM 51-40- - [SDR FDEA202105201334](https://openairdocs.org/sdr/FDEA202105201334), May 20, 2021: GIRT BAR. DISENGAGED. WHEN OPENING R1 DOOR NOTED GIRT BAR HANGING DOWN FROM BOTTOM OF DOOR. COMPLIED WITH B757 AMM 25-66-10-2 PAGES 14-15 STEPS 14-21. RENEGAGED THE GIRT BAR CAMS IN - [SDR FDEA202012313226](https://openairdocs.org/sdr/FDEA202012313226), Dec 31, 2020: ACTUATOR. MALFUNCTIONED. GEAR DISAGREE WHEN LANDING GEAR LEVER SELECTED DOWN BEFORE LANDING. NOSE GEAR INDICATED UNSAFE. RAN QRH FOR GEAR DISAGREE AND EXTENDED GEAR VIA ALTERNATE EXTENS - [SDR FDEA202012243205](https://openairdocs.org/sdr/FDEA202012243205), Dec 24, 2020: GATE. CORRODED. L1 DOOR LOWER GATE LOWER EDGE PITTED ACCOMPLISHED EA NR F-5210-T0358769. DOORS-PASSENGER/CREW-NR 1 PASS, DOOR LOWER GATE, EDGE PITTING. - [SDR FDEA202012223200](https://openairdocs.org/sdr/FDEA202012223200), Dec 22, 2020: SHELF. CRACKED. E&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007. - [SDR FDEA202012223199](https://openairdocs.org/sdr/FDEA202012223199), Dec 22, 2020: MOUNT. CRACKED. E&E COMPARTMENT E3-1 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007. - [SDR FDEA202012223197](https://openairdocs.org/sdr/FDEA202012223197), Dec 22, 2020: FLANGE. CRACKED. E&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT FLANGE CRACKED. REMOVED AND REPLACED FLANGE, IAW B SRM 51-40-02 AND DWG NR 284N1028 REV C. - [SDR FDEA202012173180](https://openairdocs.org/sdr/FDEA202012173180), Dec 17, 2020: SKIN. CRACKED. NOSE WHEEL WELL RT DOOR CUT OUT UPPER SKIN STRIP IS CRACKED AT BS 324 RBL 19. REMOVED AND REPLACED STRIP, PER DWG 141N0094. - [SDR FDEA202011102805](https://openairdocs.org/sdr/FDEA202011102805), Nov 10, 2020: ACTUATOR. FAILED. PDIS 994 32-30 8627 10NOV20 IND OPEN U. GEAR DISAGREE AND GEAR DOORS EICAS FOR 90 SECONDS UNTIL GEAR FULLY RETRACTED AND EICAS MESSAGES. NOISE FROM NOSE GEAR AR - [SDR FDEA2020070211406](https://openairdocs.org/sdr/FDEA2020070211406), Jul 1, 2020: CLAMP. WORN. LEFT BLEED DUCT LEAK AT FL 370 WITH ENGINE ANTI-ICE ON. COMPLETED QRH AND SECURED ENGINE ANTI-ICE AND LIGHT WENT OUT WITH NO SECONDARIES. REMOVED STAND OFF CLAM - [SDR FDEA2020070201409](https://openairdocs.org/sdr/FDEA2020070201409), Jun 30, 2020: CLAMP. WORN. LEFT BLEED DUCT LEAK AT FL 370 WITH ENGINE ANTI-ICE ON. COMPLETED QRH AND SECURED ENGINE ANTI-ICE AND LIGHT WENT OUT WITH NO SECONDARIES. ACCOMPLISHED WING AND - [SDR FDEA2019121303214](https://openairdocs.org/sdr/FDEA2019121303214), Dec 10, 2019: PROXIMITY SENSOR. INOPERATIVE. RIGHT DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. VERIFIED 28VAC AT SLIDE LIGHT L404. VERIFIED GOOD CONTINUITY THROUGH AFT GIRT BAR PROX SENSOR S10217 WITH - [SDR FDEA201911263110](https://openairdocs.org/sdr/FDEA201911263110), Nov 26, 2019: LIGHT. INOPERATIVE. PDIS 994 25-60 7876 26NOV19 BUF OPEN U LOGPAGES:3167525 R1 DOOR SLIDE LIGHT NOT ILLUMINATED WHILE ARMED. MEL 26NOV19 00:00 BUF U RELEASED FOR SERVICE PER MEL : - [SDR FDEA201812153509](https://openairdocs.org/sdr/FDEA201812153509), Dec 15, 2018: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK STA 1540 RBL 45.7 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIG MAT .075 REM .050 LOSS .025 FOUND OUT OF LIMITS IAW SRM 53-00-52 - [SDR FDEA201812133498](https://openairdocs.org/sdr/FDEA201812133498), Dec 13, 2018: CREASE BEAM. CORRODED. MAIN CABIN LBL 62 CREASE BEAM AT STA 800 HAS CORROSION. REMOVED CORROSION ON CREASE BEAM STA 800 LBL 62 IAW B757 SRM 51-10-02. ORIG MAT .071 REM .051 LOSS .020 - [SDR FDEA201812113493](https://openairdocs.org/sdr/FDEA201812113493), Dec 11, 2018: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK LBL 24.75 AT STA 618 HAS CORROSION. REMOVED CORROSON ON SEAT TRACK STA 618 LBL 24.75 IAW B757 SRM 51-10-02. ORIG MAT .070 REM .035 LOSS .0 - [SDR FDEA201812113492](https://openairdocs.org/sdr/FDEA201812113492), Dec 11, 2018: FLOORBEAM. CORRODED. MAIN CABIN FLOOR SUPPORT BTWN LBL 24.75 / BL 0 AT BS 1020 CORROSION. REMOVED CORR ON FLOOR SUPPORT BETWEEN LBL 24.75 / BL0 STA. 1020 IAW B757 SRM 51-10 10-02. F - [SDR FDEA201812113491](https://openairdocs.org/sdr/FDEA201812113491), Dec 11, 2018: SEAT TRACK. CORRODED. CORROSION IN THE MAIN CABIN SEAT TRACK, RT FLANGE UPPER SURFACE, BETWEEN BS 1020 TO BS 1040 LBL 58. REMOVED CORR ON SEAT TRACK STA 1020 TO 1040 LBL58 IAW SRM 51 - [SDR FDEA201812053436](https://openairdocs.org/sdr/FDEA201812053436), Dec 5, 2018: FLOORBEAM. CRACKED. STUB BEAM IN FORWARD CARGO AT STA 580 AND LBL 45. COMPLIED WITH MAINFRAME STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR AT LBL 45. - [SDR FDEA201808172067](https://openairdocs.org/sdr/FDEA201808172067), Aug 17, 2018: CONTROLLER. MALFUNCTIONED. AT FL 340, NOTICED EARS POPPING. LOOKED AT THE CABIN ALTITUDE INDICATOR & IT INDICATED NORMAL, THE RATE GAUGE FLUCTUATED. AFTER A FEW MINUTES, THE RIGHT PACK IN - [SDR FDEA201806231573](https://openairdocs.org/sdr/FDEA201806231573), Jun 23, 2018: CHARGER. INOPERATIVE. RT EMERGENCY EXIT SIGN DID NOT TEST, LAMPS OUT/MISSING. REMOVED AND REPLACED BATTERY PACK/ CHARGER TRAY FOR RT EMERGENCY EXIT SIGN, REF AMM 33-51-07-2. OPS CHEC - [SDR FDEA201801120083](https://openairdocs.org/sdr/FDEA201801120083), Jan 12, 2018: LOCK. OUT OF ADJUST. LEFT FORWARD ENTRY DOOR WAS DISARMED THEN OPENED. PARTS FELL OFF DOOR AND SLIDE PARTIALLY HANGING OUT. INSTALLED THE AFT BAR LOCK ONTO GIRT BAR IAW MM 25-66-01- - [SDR FDEA201709032454](https://openairdocs.org/sdr/FDEA201709032454), Sep 3, 2017: GIRT BAR. DISLODGED. RT DOOR SLIDE LIGHT IS INOP. DURING T/S FOUND THAT THE GIRT BAR WAS DISLODGED FROM DOOR. REINSTALLED GIRT BAR ON DOOR REF AMM 25-66-10-2-0. OPS CHECKS GOOD. SLI - [SDR FDEA201708052124](https://openairdocs.org/sdr/FDEA201708052124), Aug 5, 2017: SENSOR. DIRTY. SLIDE ARMED INDICATOR LIGHT ON R FWD ENT DOOR DOES NOT ILLUMINATE. INSPECTED GIRT BAR DETECTION PER AMM 25_66_11_2_0. SOME DEBRIS NOTED, CLEANED SENSOR AREA. OP - [SDR FDEA201707061860](https://openairdocs.org/sdr/FDEA201707061860), Jul 6, 2017: BOTTLE. LOW PRESSURE. FOUND THE L1 DOOR ASSIST BOTTLE PRESSURE LOW R & R THE L1 DOOR ASSIST BOTTLE IAW AMM 52-11-30-4. - [SDR FDEA201705051360](https://openairdocs.org/sdr/FDEA201705051360), May 5, 2017: PDU. TRIPPED. TE FLAP DISAGREE MESSAGE AFTER SELECTING FLAPS 20 ON VISUAL APPROACH. QRH COMPLETED AND LANDED FLAPS 20. TROUBLESHOT TE FLAP DISAGREE IAW FIM 27-51 FT 808. FOUN - [SDR FDEA201611224199](https://openairdocs.org/sdr/FDEA201611224199), Nov 22, 2016: FRAME. DENTED. AFT CARGO FRAME AT BS 1340 HAS A DENT BETWEEN STRINGERS 25L AND 26L. REPAIRED IAW EA F-5310-T0329984 P1. MAJOR REPAIR. - [SDR FDEA201611224200](https://openairdocs.org/sdr/FDEA201611224200), Nov 22, 2016: FRAME. DENTED. AFT CARGO BAY FRAME AT BS 1420 HAS A DENT ABOVE STRINGER 26L. COMPLIED WITH EA F-5310-T0329906 P1. - [SDR FDEA201611154022](https://openairdocs.org/sdr/FDEA201611154022), Nov 15, 2016: WEB. CORRODED. MAIN CARGO WEB AT BS 4121 RBL 67, FOUND CORRODED, UPPER RT CORNER. REMOVED AND REPLACED THE WEB IAW DRAWING 146N5590 REV E. - [SDR FDEA201610043454](https://openairdocs.org/sdr/FDEA201610043454), Oct 4, 2016: GIRT BAR. DAMAGED. L1 DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE. THE GIRT BAR WILL NOT FULLY ENGAGE. R & R THE GIRT BAR IAW MM 25-66-10-2. PERFORMED ADJUSTMENT AND TEST IAW MM 25 - [SDR FDEA201302210387](https://openairdocs.org/sdr/FDEA201302210387), Feb 21, 2013: CONTROL PANEL. MALFUNCTIONED. EMERGENCY EXIT LIGHT CONTROL PANEL "UNARMED" ANNUNCIATOR INOPERATIVE. R & R OVERHEAD EMERGENCY EXIT LIGHTS CONTROL PANEL IAW AMM 33-51-08, OPS CHECKED NORMAL. - [SDR FDEA201211154040](https://openairdocs.org/sdr/FDEA201211154040), Nov 15, 2012: SUPPORT ANGLE. CRACKED. ANGLE CRACKED NR 1 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INS - [SDR FDEA201211154039](https://openairdocs.org/sdr/FDEA201211154039), Nov 15, 2012: ANGLE. CRACKED. ANGLE CRACKED NR 2 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INS - [SDR FDEA201208163017](https://openairdocs.org/sdr/FDEA201208163017), Aug 16, 2012: LINER. OUT OF POSITION. WHEN ARMING L1 DOOR, EXCESSIVE FORCE HAD TO BE APPLIED TO GET SLIDE ARM INDICATOR TO DISPLAY. FOUND ESCAPE SLIDE ARMING TAB RUBBING ON LOWER LINING OF L1 DOOR. - [SDR FDEA201203130910](https://openairdocs.org/sdr/FDEA201203130910), Mar 13, 2012: LIGHT. INOPERATIVE. R1 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. R & R R1 EXTERIOR SLIDE LIGHT IAW AMM 33-51-06-2-1. OPS CHECKED GOOD. ACFT OK FOR SERVICE. - [SDR FDEA201109224036](https://openairdocs.org/sdr/FDEA201109224036), Sep 22, 2011: GIRT BAR. OUT OF ADJUST. R1 DOOR SLIDE ARMING LEVER IS BINDING BEFORE IT GOES FULL TRAVEL TO ARM. ORIGINAL GSP-LINE. ADJUSTED GIRT BAR FLOOR FITTINGS PER MM 52-11-25-5-0. OPS CHECKED GO - [SDR FDEA201109153891](https://openairdocs.org/sdr/FDEA201109153891), Sep 15, 2011: PANEL. LOOSE. PANEL BEHIND ARMED/DISARMED SLIDE ON LT DOOR IS LOOSE. REMOVED THE L-1 DOOR INTERIOR COVER. INSTALLED THE NEW PLATE RETAINER RAIL IAW AMM 52-11-02 & SRM 51-70-0 - [SDR FDEA201108093143](https://openairdocs.org/sdr/FDEA201108093143), Aug 9, 2011: BATTERY PACK. FAILED. EMERGENCY EXIT LIGHTS WILL NOT TEST. EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. - [SDR FDEA201106292483](https://openairdocs.org/sdr/FDEA201106292483), Jun 29, 2011: ENGINE. ERRATIC. AT CRUISE FL 400, THE RT ENGINE BECAME ERRATIC WITH EPR FLUCTUATIONS BETWEEN 1.10 TO 1.29 WITH ASSOCIATED VARIATIONS IN N1 AND FUEL FLOW. TURNED AUTO THROTTLES - [SDR FDEA201105171850](https://openairdocs.org/sdr/FDEA201105171850), May 17, 2011: EEC. MALFUNCTIONED. ON DESCENT INTO MEM GOT RT ENG OIL PRESS ALERT WITH OIL PRESS ABOVE 70 PSI (RED) SHUTDOWN RT ENGINE IAW QRH. RECIEVED STATUS MESSAGES, RT ENG SEC SEL RT ENG LOW - [SDR FDEA201012094622](https://openairdocs.org/sdr/FDEA201012094622), Dec 9, 2010: SUPPORT. CHAFED. LT WING- L/E WING APPROX W/S 240 - L/E DUCT SUPPORT CHAFING INTO VERTICAL SUPPORT. REMOVED & INSTALLED NEW STIFFNER IAW SRM 51-40-02. RECIEVED NEW STIFFNER ON T - [SDR FDEA201012064598](https://openairdocs.org/sdr/FDEA201012064598), Dec 6, 2010: SKIN. WORN. LT WING OTBD MAIN FLAP L/E INBD SIDE HAS A WORN SECTION APPROX 10" LONG . EVALUATED LT WING OTBD MAIN FLAP AND FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, PG 10 - [SDR FDEA201011264496](https://openairdocs.org/sdr/FDEA201011264496), Nov 26, 2010: SKIN. DENTED. EXTERNAL FUSELAGE SKIN STA 1720-1740 BETWEEN S-25R TO S-16R HAS DENT AT LAP SEAM. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO LAP SEAM. REP - [SDR FDEA201011184419](https://openairdocs.org/sdr/FDEA201011184419), Nov 18, 2010: SKIN. DAMAGED. LT WING AILERON OTBD AREA LWR SURFACE PUNCTURED THRU SKIN DIAMETER OF HOLE 0.250 BY 1"X1" REPAIRED LT WING AILERON OTBD AREA IAW SRM 51-70-17 SB 757-51-0006 IAW - [SDR FDEA201011184421](https://openairdocs.org/sdr/FDEA201011184421), Nov 18, 2010: WEDGE. CHAFED. NR 6 SLAT T/E WEDGE UNDER SKIN HAS CHAFE MARKS, REPAIRED NR6 SLAT T/E IAW SRM 51-70-10 IAW SRM 57-43-02. DAMAGE WAS LOCATED AT STA 177.5, APPROX 3" FWD OF T/E. - [SDR FDEA201011184420](https://openairdocs.org/sdr/FDEA201011184420), Nov 18, 2010: SKIN. DAMAGED. LT WING NR 2 SLAT HAS NUMEROUS CHAFED MARKS ALONG BOTTOM SKIN AFT EDGE REPAIRED LT WING NR 2 SLAT IAW SRM 51-70-10 IAW SRM 57-43-02 DAMAGE LOCATED AT STA 652.50 - [SDR FDEA201010274180](https://openairdocs.org/sdr/FDEA201010274180), Oct 27, 2010: GATE. CORRODED. L1 LOWER GATE PANEL HAS SEVERE CORROSION ALONG LOWER EDGE AND ON GATE SKIN PANEL AT LOWER EDGE. REMOVED AND REPLACED L1 DOOR LOWER GATE ASSY, PER AMM 52-11-38. - [SDR FDEA201010103984](https://openairdocs.org/sdr/FDEA201010103984), Oct 10, 2010: SEAT TRACK. CORRODED. AT RBL 24, BL 1600- 1640 HAS HEAVY PITTING IN INBD RADIUS OF SEAT TRACK CROWN TO FLANGE. CHECKED LIMITS FOUND TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 10 - [SDR FDEA201009223634](https://openairdocs.org/sdr/FDEA201009223634), Sep 22, 2010: SKIN. DENTED. PREVIOUS SKIN DENTED AT BS 309, S18L. ACCOMPLISHED SKIN REPAIR IAW EA F-5330-141203, BS 309, BELOW S17L. DENT WAS OUT OF LIMITS DUE TO PROXIMITY TO BS 310.5 FRA All 72: https://openairdocs.org/aircraft/N994FD/reports.md ## STCs that may be installed (OpenAirDocs) (5) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Boeing 757-23A) - [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 757 Series - [STC ST01675CH](https://openairdocs.org/stc/ST01675CH): Installation of Butterfly Valve Ring AIR23028 in starter control valves, part number 775538 or 799700. Cook Airtomic. Lists 757 Series - [STC ST02296AT](https://openairdocs.org/stc/ST02296AT): Upgrade existing HF Voice Communication System to provide HF datalink capability. ARINC, Inc. Lists 757 Series - [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 757 Series - [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 757 Series ## Related - Other Boeing 757-23A aircraft: https://openairdocs.org/model/boeing-757-23a/aircraft.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.